EP2134884A2 - Procédé d'application d'un revêtement à résistance élevée sur des pièces à usiner et/ou des matériaux - Google Patents
Procédé d'application d'un revêtement à résistance élevée sur des pièces à usiner et/ou des matériauxInfo
- Publication number
- EP2134884A2 EP2134884A2 EP08736109A EP08736109A EP2134884A2 EP 2134884 A2 EP2134884 A2 EP 2134884A2 EP 08736109 A EP08736109 A EP 08736109A EP 08736109 A EP08736109 A EP 08736109A EP 2134884 A2 EP2134884 A2 EP 2134884A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- coating
- layer
- workpiece
- materials
- workpieces
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000576 coating method Methods 0.000 title claims abstract description 106
- 239000011248 coating agent Substances 0.000 title claims abstract description 87
- 239000000463 material Substances 0.000 title claims abstract description 76
- 238000000034 method Methods 0.000 title claims abstract description 68
- 239000010410 layer Substances 0.000 claims abstract description 121
- 239000012790 adhesive layer Substances 0.000 claims abstract description 23
- 239000007789 gas Substances 0.000 claims description 50
- 238000004544 sputter deposition Methods 0.000 claims description 25
- 239000000843 powder Substances 0.000 claims description 21
- 239000012495 reaction gas Substances 0.000 claims description 18
- 238000007743 anodising Methods 0.000 claims description 14
- 238000010285 flame spraying Methods 0.000 claims description 14
- 230000007704 transition Effects 0.000 claims description 11
- 239000000919 ceramic Substances 0.000 claims description 8
- 238000001962 electrophoresis Methods 0.000 claims description 7
- 238000009713 electroplating Methods 0.000 claims description 6
- 239000000853 adhesive Substances 0.000 claims description 5
- 230000001070 adhesive effect Effects 0.000 claims description 5
- 239000012298 atmosphere Substances 0.000 claims description 5
- 229910052593 corundum Inorganic materials 0.000 claims description 5
- 239000010431 corundum Substances 0.000 claims description 5
- 230000005672 electromagnetic field Effects 0.000 claims description 5
- 238000007750 plasma spraying Methods 0.000 claims description 5
- 230000003213 activating effect Effects 0.000 claims description 2
- JOPOVCBBYLSVDA-UHFFFAOYSA-N chromium(6+) Chemical compound [Cr+6] JOPOVCBBYLSVDA-UHFFFAOYSA-N 0.000 claims description 2
- 230000008569 process Effects 0.000 description 16
- 229910052751 metal Inorganic materials 0.000 description 15
- 239000002184 metal Substances 0.000 description 15
- 238000005520 cutting process Methods 0.000 description 14
- 239000000758 substrate Substances 0.000 description 13
- 239000000203 mixture Substances 0.000 description 12
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 11
- 238000000151 deposition Methods 0.000 description 11
- 230000008021 deposition Effects 0.000 description 11
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 10
- 229910052799 carbon Inorganic materials 0.000 description 10
- 239000001301 oxygen Substances 0.000 description 10
- 229910052760 oxygen Inorganic materials 0.000 description 10
- 229910045601 alloy Inorganic materials 0.000 description 9
- 239000000956 alloy Substances 0.000 description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- 229910052782 aluminium Inorganic materials 0.000 description 8
- 229910052710 silicon Inorganic materials 0.000 description 8
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 7
- 229910000831 Steel Inorganic materials 0.000 description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 7
- 238000006243 chemical reaction Methods 0.000 description 7
- 238000000623 plasma-assisted chemical vapour deposition Methods 0.000 description 7
- 239000010703 silicon Substances 0.000 description 7
- 239000010959 steel Substances 0.000 description 7
- 239000010936 titanium Substances 0.000 description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 6
- 239000004033 plastic Substances 0.000 description 6
- 229920003023 plastic Polymers 0.000 description 6
- 238000004080 punching Methods 0.000 description 6
- 229910052718 tin Inorganic materials 0.000 description 6
- 239000011135 tin Substances 0.000 description 6
- 229910052719 titanium Inorganic materials 0.000 description 6
- 230000008901 benefit Effects 0.000 description 5
- 239000011651 chromium Substances 0.000 description 5
- 239000002131 composite material Substances 0.000 description 5
- 229910052802 copper Inorganic materials 0.000 description 5
- 239000010949 copper Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 150000002739 metals Chemical class 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 4
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 4
- 238000002048 anodisation reaction Methods 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 4
- 238000007749 high velocity oxygen fuel spraying Methods 0.000 description 4
- 150000002500 ions Chemical class 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 229910052750 molybdenum Inorganic materials 0.000 description 4
- 229910052759 nickel Inorganic materials 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 238000002161 passivation Methods 0.000 description 4
- 239000012071 phase Substances 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 3
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 3
- 229910052786 argon Inorganic materials 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000005229 chemical vapour deposition Methods 0.000 description 3
- 229910017052 cobalt Inorganic materials 0.000 description 3
- 239000010941 cobalt Substances 0.000 description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 3
- 238000005553 drilling Methods 0.000 description 3
- 239000002737 fuel gas Substances 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 150000001247 metal acetylides Chemical class 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- LIVNPJMFVYWSIS-UHFFFAOYSA-N silicon monoxide Chemical class [Si-]#[O+] LIVNPJMFVYWSIS-UHFFFAOYSA-N 0.000 description 3
- 229910052814 silicon oxide Inorganic materials 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- FJKROLUGYXJWQN-UHFFFAOYSA-N 4-hydroxybenzoic acid Chemical compound OC(=O)C1=CC=C(O)C=C1 FJKROLUGYXJWQN-UHFFFAOYSA-N 0.000 description 2
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 description 2
- 229910009043 WC-Co Inorganic materials 0.000 description 2
- 230000004913 activation Effects 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 239000012459 cleaning agent Substances 0.000 description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 2
- 230000005684 electric field Effects 0.000 description 2
- 238000004070 electrodeposition Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 150000002431 hydrogen Chemical class 0.000 description 2
- 239000000976 ink Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000005055 methyl trichlorosilane Substances 0.000 description 2
- JLUFWMXJHAVVNN-UHFFFAOYSA-N methyltrichlorosilane Chemical compound C[Si](Cl)(Cl)Cl JLUFWMXJHAVVNN-UHFFFAOYSA-N 0.000 description 2
- 238000003801 milling Methods 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- 229910052756 noble gas Inorganic materials 0.000 description 2
- 150000002835 noble gases Chemical class 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 239000011241 protective layer Substances 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 229910000077 silane Inorganic materials 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 238000000992 sputter etching Methods 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- VXUYXOFXAQZZMF-UHFFFAOYSA-N titanium(IV) isopropoxide Chemical compound CC(C)O[Ti](OC(C)C)(OC(C)C)OC(C)C VXUYXOFXAQZZMF-UHFFFAOYSA-N 0.000 description 2
- UHUUYVZLXJHWDV-UHFFFAOYSA-N trimethyl(methylsilyloxy)silane Chemical compound C[SiH2]O[Si](C)(C)C UHUUYVZLXJHWDV-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 229940090248 4-hydroxybenzoic acid Drugs 0.000 description 1
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 1
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 239000004166 Lanolin Substances 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 235000002595 Solanum tuberosum Nutrition 0.000 description 1
- 244000061456 Solanum tuberosum Species 0.000 description 1
- 239000004809 Teflon Substances 0.000 description 1
- 229920006362 Teflon® Polymers 0.000 description 1
- 229910010413 TiO 2 Inorganic materials 0.000 description 1
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- AMXBISSOONGENB-UHFFFAOYSA-N acetylene;ethene Chemical compound C=C.C#C AMXBISSOONGENB-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 125000003368 amide group Chemical group 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000003266 anti-allergic effect Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 125000004429 atom Chemical group 0.000 description 1
- 210000000988 bone and bone Anatomy 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000001311 chemical methods and process Methods 0.000 description 1
- 238000009388 chemical precipitation Methods 0.000 description 1
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 description 1
- 229910000423 chromium oxide Inorganic materials 0.000 description 1
- 238000005345 coagulation Methods 0.000 description 1
- 230000015271 coagulation Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 210000002808 connective tissue Anatomy 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- MROCJMGDEKINLD-UHFFFAOYSA-N dichlorosilane Chemical compound Cl[SiH2]Cl MROCJMGDEKINLD-UHFFFAOYSA-N 0.000 description 1
- 125000000118 dimethyl group Chemical group [H]C([H])([H])* 0.000 description 1
- 239000002270 dispersing agent Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000010494 dissociation reaction Methods 0.000 description 1
- 230000005593 dissociations Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000010292 electrical insulation Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 238000000635 electron micrograph Methods 0.000 description 1
- 238000001652 electrophoretic deposition Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- -1 gasified kerosene Chemical compound 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-M hydroxide Chemical compound [OH-] XLYOFNOQVPJJNP-UHFFFAOYSA-M 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000007943 implant Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 229940039717 lanolin Drugs 0.000 description 1
- 235000019388 lanolin Nutrition 0.000 description 1
- 238000002386 leaching Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910021645 metal ion Inorganic materials 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- CWQXQMHSOZUFJS-UHFFFAOYSA-N molybdenum disulfide Chemical compound S=[Mo]=S CWQXQMHSOZUFJS-UHFFFAOYSA-N 0.000 description 1
- 210000003205 muscle Anatomy 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- SIWVEOZUMHYXCS-UHFFFAOYSA-N oxo(oxoyttriooxy)yttrium Chemical compound O=[Y]O[Y]=O SIWVEOZUMHYXCS-UHFFFAOYSA-N 0.000 description 1
- 125000004430 oxygen atom Chemical group O* 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- NFHFRUOZVGFOOS-UHFFFAOYSA-N palladium;triphenylphosphane Chemical compound [Pd].C1=CC=CC=C1P(C=1C=CC=CC=1)C1=CC=CC=C1.C1=CC=CC=C1P(C=1C=CC=CC=1)C1=CC=CC=C1.C1=CC=CC=C1P(C=1C=CC=CC=1)C1=CC=CC=C1.C1=CC=CC=C1P(C=1C=CC=CC=1)C1=CC=CC=C1 NFHFRUOZVGFOOS-UHFFFAOYSA-N 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 239000004645 polyester resin Substances 0.000 description 1
- 229920001225 polyester resin Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 229920005749 polyurethane resin Polymers 0.000 description 1
- 229910052573 porcelain Inorganic materials 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 235000012015 potatoes Nutrition 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000007639 printing Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 239000005871 repellent Substances 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 238000007788 roughening Methods 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 229910021332 silicide Inorganic materials 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 210000003491 skin Anatomy 0.000 description 1
- 238000003307 slaughter Methods 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 238000004901 spalling Methods 0.000 description 1
- 229910002076 stabilized zirconia Inorganic materials 0.000 description 1
- 230000001954 sterilising effect Effects 0.000 description 1
- 238000004659 sterilization and disinfection Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 230000002123 temporal effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000007751 thermal spraying Methods 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- 229910003470 tongbaite Inorganic materials 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 1
- NXHILIPIEUBEPD-UHFFFAOYSA-H tungsten hexafluoride Chemical compound F[W](F)(F)(F)(F)F NXHILIPIEUBEPD-UHFFFAOYSA-H 0.000 description 1
- 239000012808 vapor phase Substances 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/02—Pretreatment of the material to be coated
- C23C16/0272—Deposition of sub-layers, e.g. to promote the adhesion of the main coating
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/02—Pretreatment of the material to be coated
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/02—Pretreatment of the material to be coated
- C23C16/0272—Deposition of sub-layers, e.g. to promote the adhesion of the main coating
- C23C16/029—Graded interfaces
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
- C23C16/26—Deposition of carbon only
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/455—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/455—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for introducing gases into reaction chamber or for modifying gas flows in reaction chamber
- C23C16/45523—Pulsed gas flow or change of composition over time
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/28—Web or sheet containing structurally defined element or component and having an adhesive outermost layer
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/28—Web or sheet containing structurally defined element or component and having an adhesive outermost layer
- Y10T428/2848—Three or more layers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
Definitions
- the present invention relates to a method for applying a coating to workpieces and / or materials according to the preamble of claim 1.
- Such coatings are applied to workpieces and / or materials in particular by plasma coating methods such as the "Plasma Enhanced Chemical Vapor Deposition” (PECVD) method.
- PECVD Plasma Enhanced Chemical Vapor Deposition
- This process is a special form of "Chemical Vapor Deposition” (CVD), in which the deposition of thin layers by chemical reaction takes place in a vacuum chamber; In this case, the material with which the coating is to be carried out, in the gas or vapor phase before.
- PECVD is supported by a plasma.
- a strong electric field is applied between the substrate to be coated and a counter electrode, through which a plasma is ignited.
- the plasma causes a breakdown of the bonds of the reaction gas and decomposes it into ions or radicals, which precipitate on the substrate and cause the chemical precipitation reaction there.
- a higher deposition rate can be achieved at a lower deposition temperature than with CVD.
- This type of coating is therefore particularly suitable for punching, cutting, drilling and screwing tools, cutting tools, prostheses, ball or roller bearings, gears, pinions, drive chains, sound and drive units in magnetic recording devices, as well as surgical and dental surgical instruments.
- it is suitable for blades with exchangeable blades, e.g. surgical knives, and / or blades and / or knives for industrial applications.
- the workpieces to be coated and / or materials may in particular consist of metals, ceramics or plastics, have such materials, or else represent mixtures or composites of said materials.
- the workpieces and / or materials to be coated have a different residual stress than the coating. This is due to the nature of the production. For example, hard metal workpieces or materials suffer from extreme internal stress or, depending on the composition, are subject to very high residual stresses during the flame spraying process.
- powder mixtures are used, which in the way do not allow a subsequent DLC coating in the true sense, these repel even if they must be carbon-free or should.
- HSS HSS
- Object of the present invention is therefore to provide a well-adherent coating for workpieces and / or materials that gives them on the surface a high hardness, high toughness, high resistance to tribological stresses, high smoothness and a low coefficient of friction, and which is also resistant to point loads.
- Another object of the present invention is to provide a well-adherent coating for workpieces and / or materials which is resistant to point loads and at the same time has suitable surface properties with respect to surface tension and resistance to paints and cleaning agents such as acids and alkalis, electrical insulating and heat-conducting properties , and / or has biocompatibility and antiallergic properties.
- Another object of the present invention is to provide a well-adherent coating for cutting, chip, drilling, forging, milling, screwing and punching tools, which has a long service life and / or life.
- Another object of the present invention is to provide a well-adhering life and / or life-prolonging coating which is suitable for blades having a high sharpness.
- a method for applying a coating to workpieces and / or materials comprising the following steps:
- the workpiece or material may consist in particular of ceramic, iron, steel, high-alloy steel, nickel, cobalt and their alloys with chromium, molybdenum and aluminum, copper and copper alloys, titanium or alloys comprising the aforementioned materials. Furthermore, the workpiece or the material of metals and / or metallic alloys based on Zn, Sn, Cu, Fe, Ni, Co, Al, Ti, and the refractory metals such as Mo, W, Ta etc . Next come sintered metal materials and Metal-ceramic composites (MMC) and metal-polymer composites as well as ceramic materials of oxides, carbides, borides and nitrides in question.
- MMC Metal-ceramic composites
- the workpiece may also consist of plastic or a plastic mixture.
- plastic or a plastic mixture.
- alloys or composites of the mentioned materials come into question.
- the high-strength cover layer is applied by plasma coating.
- a carbon- or silicon-containing reaction gas such as methane (CH 4 ), ethene (C 2 H 4 ), acetylene (C 2 H 2 ), methyl-trichloro-silane (CH 3 SiCl 3 ) or tetramethyldisiloxane (C 4 H 14 OSi 2 ).
- a carbonaceous overcoat which often has diamond-like properties and structures and is therefore also referred to as a diamond-like carbon (DLC) layer
- DLC diamond-like carbon
- a silicon nitride film as a cap layer is formed by using the reaction gases ammonia and dichlorosilane.
- the reaction gases silane and oxygen are used.
- Such layers are also particularly preferred embodiments of the invention.
- tungsten hexafluoride (WF 6 ) is used as the reaction gas, for example.
- Titanium nitride layers as a topcoat for hardening tools are made of TDMAT (Tetrakis dimethyl amido titanium) and nitrogen. Silicon carbide layers are deposited from a mixture of hydrogen and methyl trichlorosilane (CH 3 SiCIs).
- titanium-containing layers wherein as the starting material preferably titanium isopropoxide (Ci 2 H 2S O 4 Ti) is used.
- the adhesive layer of the invention contributes in various ways to improved adhesion of the cover layer on the workpiece or material. So
- the intermediate layer is applied with the residual stress verquer to the residual stress of the material, ie the substrate and thus has a balancing effect.
- the workpiece to be coated or the material to be coated consists of metal, in particular of steel or stainless steel, aluminum or titanium and their alloys.
- the surface of these metals is relatively soft and easily plastically deformable compared to the applied high strength carbon or silicon containing overcoat.
- the said cover layer is extremely hard, but it is brittle. In some situations, for example extremely high point loads, this leads to the workpiece or the material being plastically deformed and the cover layer, due to its brittleness, can not follow this deformation, but it breaks or bursts.
- Tools and materials that are coated with such a top layer so have in certain applications and load scenarios low lifetimes and / or life.
- support layers do not exhibit the extreme hardness of the cover layer, but have sufficiently tough properties that they do not yield at high point loads, thus preventing breakage or spalling of the cover layer.
- the properties of said support layer will be discussed below.
- step b) the step
- step a.2) can therefore be carried out before and / or after the step a.1).
- sputtering or “sputter etching” refers to a physical process in which atoms are dissolved out of a solid by bombardment with high-energy ions and pass into the gas phase. These ions are often - similar to the PECVD - by generating a plasma by means of a high-frequency alternating electromagnetic field in a vacuum chamber generated.
- noble gases are generally suitable as the reaction gas, for example argon (Ar 2 ).
- Ar 2 argon
- oxygen (O 2 ) for non-ferrous materials such as brass, bronze, aluminum etc. a mixture of oxygen (O 2 ) and hydrogen (H 2 ).
- a mixture of H 2 and O 2 is also used if the subsequent intermediate layer or the substrate to be coated requires it.
- Ion etching allows the substrate surface to be cleaned down to the nanoscale and removed in a nominal sense. This removal of the surface can be measured, for example, with the aid of O 2 after a short time and moves per hour in the range of 100 nm. This ensures that the substrate surface to be treated is free of all impurities.
- the use for cleaning the surface in the broadest sense even the activation, by a mixture of H 2 and O 2 necessary to achieve any adhesion.
- said support layer by at least one method selected from the group
- the heat to melt the powder is by the reaction of oxygen and fuel gas, such as gasified kerosene, in the Combustion chamber generated.
- the temperatures reached in the flame are up to about 3000 0 C.
- the reaction expands the gas and accelerates the spray powder to a high speed.
- a plasma torch In plasma spraying, a plasma torch is usually used in which an anode and cathode are separated by a narrow gap. A DC voltage creates an arc between the anode and the cathode. The gas flowing through the plasma torch is passed through the arc and thereby ionized. The ionization, or subsequent dissociation, generates a highly heated (up to 20,000 K), electrically conductive gas of positive ions and electrons. In this Plasmajet produced powder is injected, which is melted by the high plasma temperature. The plasma gas stream entrains the powder particles and hurls them at a speed of up to 1000 m / s onto the workpiece to be coated.
- the gas molecules return to a stable state after only a short time, no longer release any energy, and so the plasma temperature drops again after a short distance.
- the plasma coating is usually carried out under atmospheric pressure.
- Gases used are argon, helium, hydrogen, oxygen or nitrogen.
- Flame spraying with powder is the oldest method of thermal spraying technology. Due to the fuel gas / oxygen flame as a heat source only low melting metals and alloys can be processed. By flame spraying with subsequent melting of e.g. Nickel- or cobalt-based hard alloys can achieve dense and thick layers up to 2.5 mm. Additions of carbides cause a significant increase in hardness.
- the coating material is present as a powder.
- metal-bound carbides such as tungsten carbide, chromium carbide, titanium carbide, silicon carbide, or oxides, such as aluminum oxide, titanium dioxide, chromium oxide, magnesium oxide, zirconium oxide and their alloys and mixtures.
- the coating material is present as a wire.
- the coating material is applied by the fuel gas / oxygen flame and the gas velocity.
- Typical coating materials in this process are metals, eg molybdenum, Cr steel, Cr-Ni steel, Zn, etc.
- Anodizing is a process whereby an oxide protective layer is applied to an aluminum workpiece or material, which is applied by anodic oxidation, whereby the protective layer is not deposited on the workpiece, in contrast to the galvanic coating method but by converting the uppermost metal zone into an oxide or hydroxide, a 5 to 25 micron thin layer is formed to protect the aluminum from corrosion, while the natural oxide layer of aluminum is only a few nanometers thick about 8-9 according to the hardness scale of Mohs, ie between quartz and corundum.
- Oxidation of aluminum surfaces which is produced in strongly cooled electrolytes. This coating is characterized by high wear, heat, corrosion and electrical resistance. In addition, there are good sliding properties with greatly reduced mass forces. Since the hard-enamel layer is formed from the base material itself, there are no adhesion problems. The good wear properties are due to the forming during the process of alumina from the Harteloxal- layer. Hard anodising is used for extruded profiles and turned parts as well as for pressure, sand and chill casting, forging and wrought alloys. This term encompasses several anodization techniques that can be used to produce thick (50-100 ⁇ m) and dense oxide layers at low temperature.
- Electroplating is understood to mean the electrochemical deposition of metallic precipitates on workpieces or materials. In this case, electricity is sent through an electrolytic bath.
- the metal to be applied eg copper, nickel, cobalt, manganese, chromium or certain alloys
- the electric current dissolves metal ions from the consumable electrode and stores them by reduction on the goods.
- the object to be refined is uniformly coated on all sides with copper or another metal. The longer the object is in the bath and the higher the electrical current, the stronger the metal layer becomes (eg copper layer).
- the surface hardness of the workpiece or material can be increased in this way.
- Powder coating is a coating process in which a usually electrically conductive material or a workpiece is coated with powder coatings.
- the powder is sprayed electrostatically or tribostatically on the substrate to be coated and then baked.
- the workpiece is to be degreased well and, if necessary, treated with corrosion protection.
- the baking temperatures depending on the application, vary widely. Typical baking conditions are between 140 and 200 ° C.
- Various binders are used today, but typical are powder coatings based on, for example, polyurethane, epoxy or polyester resins. Because of the
- the powder can also be applied by vortex sintering. In this case, a heated workpiece is immersed briefly in a fluidized by means of compressed air powder made of plastic. The powder melts on the surface to a
- various of the mentioned methods can also be combined.
- a combination of electrophoretic and electrodeposition in successive steps. For example, first, a ceramic layer (for example, yttrium-stabilized zirconia) electrophoretically produced on a workpiece and then sintered at 1100 0 C for an open-porous layer. The next step is then through Galvansieren example, nickel deposited in the pores of the layer. By a final thermal treatment, the connection of the composite support layer thus produced to the workpiece or the material is improved.
- a ceramic layer for example, yttrium-stabilized zirconia
- the basic principle of electrophoresis is the migration of dispersed particles in a DC electric field and their deposition on an electrode.
- ceramic powders such as yttrium oxide Y 2 O 3 and titanium oxide
- the coating is usually carried out at a DC voltage of 5 - 200 V.
- a coating substrate to be coated workpiece or the material which also acts as an electrode.
- the counter electrode consists e.g. made of graphite.
- said support layer is at least one layer selected from the group
- chromium (VI) layer • chromium (VI) layer, and / or
- An anodized layer is a layer applied by the anodizing method already mentioned. Ceramic layers can be treated with various of the mentioned methods be applied, in particular with the said spraying method and the electrophoretic method.
- a chromium (V ⁇ ) layer is usually applied by electroplating.
- Corundum layers consist of Al 2 O 3 and are considered to be the second hardest mineral with a Mohs hardness of 9 after the diamond. Corundum is considered as technical ceramics and is also applied as a coating on a workpiece or a material, for example, with the said spraying method and the electrophoretic method.
- the adhesive layer is applied by means of plasma coating on the workpiece and / or the material.
- Said adhesive layer preferably has elements from the 6th and / or 7th subgroup. Preference is given here to compounds which contain the elements Cr, Mo, W, Mn, Mg, Ti and / or Si, and in particular mixtures thereof. Likewise, the individual constituents can be distributed in graded form over the depth of the adhesive layer. Particularly preferred here is Si. As reaction gas here comes e.g. the highly volatile TMS under vacuum conditions.
- Step a.2) in this embodiment represents a multi-gas sputtering process, the advantages of which will be discussed later.
- step b) and / or step c) is carried out under an inert and / or a reducing atmosphere.
- the deposition in steps b) and / or c) can take place under a protective gas atmosphere, for example by simultaneous feeding of Ar 2 .
- the chamber is purged with a protective gas such as Ar 2 in order to displace any remaining residues of an oxidizing gas such as O 2 from the chamber and / or to initiate a rinse with nitrogen as a transfer
- step b) During the transition from step b) to step c)
- counter-rotating ramps in the context of the present invention is intended to mean that during the sputtering or PEC VD process, the minute volume of at least one reaction gas is stepped or continuously reduced while the minute volume of another gas is stepped or continuously increased becomes.
- step a.2) sputtering
- step c) PECVD
- the ramps have the effect that the deposition phases of two materials merge. In this way transition areas are created with gradually changing proportions of the various coating materials. This leads to a closer interlocking of the two layers with each other and thus e.g. to a better adhesion of the cover layer to the adhesive layer.
- the central nature of said ramps is that coordinated in time a gradual transition from at least one reaction gas to at least one other reaction gas coating medium for the intermediate layer to the coating gas for the cover layer must be adjusted fluently with a certain temporal gradient. The same may apply to the change in the bias number and possibly for further coating parameters. So it must be ensured that before each transition of the reaction gases, the chamber is raised or lowered to the desired bias value, in turn, to reduce the formation of residual stress.
- the abrupt setting of the bias value must be at least 5 seconds before the start of the setting of the gradient, but at the latest 15 seconds before the same.
- step b) to step c) can be designed, for example, so that first a silicon-containing adhesive layer is applied by plasma coating.
- a silicon-containing adhesive layer is applied by plasma coating.
- the liquid at room temperature, but under hypobaric conditions highly volatile tetramethyldisiloxane (C 4 Hi 4 OSi 2 ) is used. After a while, that will be Gas minute volume for TMS successively reduced and the gas minute volume for the Kolhenstoff ambience gas acetylene (ethene) successively increased.
- Said ramp could look like this: After an optional sputtering step (a.2), the bias voltage V ⁇ ias is raised to the height required for the coating 5 seconds before the start of the application of the intermediate layer. Thereafter, the silane-containing, vaporized gas TMS is introduced with an extremely short ramp (10 s). After the adhesive layer deposition time has elapsed, the acetylene valve is gradually opened to the desired inlet value over a period of 500 seconds. At the same time, the valve for TMS gradually closes in the same time. Subsequently, the cover layer is applied over the desired time. Table 1 gives this method with exemplary values:
- the application of the cover layer can in principle take any length.
- the thickness of the cover layer grows proportionally with the duration of the coating. For this reason, the variable "X" was selected as the time value in the above table.
- ramps are driven in relation to the materials used for the adhesive layer.
- one material is successively replaced by another.
- the gas concentration in the chamber results in each case from the gas flow, the volume of the chamber and the pressure prevailing therein.
- a concentration of 0.011 results for acetylene (C 2 H 2 ) at a gas flow of 100 sccm (0.1175 g per minute) % of the chamber volume.
- a DLC layer thus prepared using acetylene as a reaction gas has a hardness of 6000-8000 HV and a thickness of 0.90 ⁇ m to 5.0 ⁇ m.
- O 2 is an attractive reaction gas for sputtering because the ionized oxygen atoms have high kinetic energy due to their high molecular weight and therefore could effectively purify a surface. In addition, oxygen is very cheap.
- O 2 comes at best for the sputtering of plastic surfaces in question, since a passivation of the surface by oxidation is not to be feared.
- a further reason for the non-use of O 2 during sputtering is for the expert when, subsequent to the sputtering, a carbon-containing layer is to be applied to the workpiece and / or the material by plasma coating. Any residual O 2 would oxidize carbon to CO and / or CO 2 , resulting in the formation of voids, gas bubbles and microcavities in the carbonaceous layer, creating a rough, less dense and less resilient surface and significantly affecting the adhesion of the topcoat ,
- Ar 2 also has disadvantages, since it results in a very rough surface during sputtering, which makes it difficult to apply a cover layer such as a DLC layer.
- the reaction gas contains in step a.2) at least temporarily the gases H 2 and O 2 .
- the H 2 contained in the reaction gas ensures that the oxidizing effect of O 2 is reduced and a passivation of the metal surfaces does not occur.
- the molecular weight of the O 2 is ideal to provide an effective cleaning effect during sputtering without, however, roughening the surface of the workpiece and / or material.
- the electromagnetic alternating field can be shut down during this time. Alternatively, it may be attempted to keep the duration of this washing step as short as possible.
- the application of the cover layer can in principle take any length.
- the thickness of the cover layer grows proportionally with the duration of the coating. For this reason, the variable "X" was selected as the time value in the above table.
- a step (a.l) may be connected for the application of a support layer.
- This step may e.g. which involves the application of a method selected from the group
- the method is carried out in a plasma coating chamber, comprising a flat high-frequency electrode for generating an alternating electromagnetic field, and a frequency generator arranged outside the chamber, characterized in that the high-frequency electrode has at least two supply lines, via which it is supplied with an alternating voltage generated by the frequency generator.
- Such a plasma coating chamber is described for the first time in the applicant's PCT / EP2007 / 057117 of the present invention.
- an alternating field with very high field strengths can be generated in the chamber.
- An alternating field generated in this way has a sufficiently high penetration depth and a high degree of homogeneity.
- homogeneous plasma in all areas of the chamber homogeneous plasma and thus achieves a homogeneous deposition rate, which manifests itself in a constant layer thickness and, as a result, in low residual stress differences within the coating thus produced. Both factors further improve the adhesion of the high-strength cover layer to be applied according to the invention.
- three or more leads are provided, as can be set in this way an even more homogeneous alternating field.
- the individual supply lines to the high-frequency electrode be adjusted separately, such that in the entire chamber, a homogeneous
- the same bias voltage is set on all controllers, which suggests identical field strengths and thus a homogeneous alternating field.
- a plasma coating chamber comprising a flat high-frequency electrode for generating an alternating electromagnetic field, a frequency generator arranged outside the chamber, and at least two leads, via which the high-frequency electrode is supplied with an alternating voltage generated by the frequency generator, for applying a coating on workpieces and / or materials according to one of the preceding method claims.
- the subject of the present invention is moreover a coating on workpieces and / or materials, comprising the following layers:
- adhesive and cover layer have a graduated transition region, or a coating on workpieces and / or materials, produced by a method according to the invention.
- said coating also has a support layer which is arranged between the workpiece and / or material and the adhesive layer.
- a support layer which is arranged between the workpiece and / or material and the adhesive layer.
- the subject of the present invention is an instrument, workpiece or material or component which is coated with one of the aforementioned methods or with an aforementioned coating.
- This instrument may be e.g. to act a surgical instrument, such as a surgical instrument. a scalpel. Likewise, this instrument can be a punching tool. Furthermore, the instrument may be e.g. to trade a butcher or slicer cutting tool
- cutting tools coated according to the invention retain their sharpness considerably longer, even if they are used under adverse circumstances. This is especially true for butchery or slaughtering cutting tools, on the one hand soft material (fat, muscle, skin, connective tissue) must cut, on the other hand, however, also hard material such as bone and frozen.
- soft material fat, muscle, skin, connective tissue
- hard material such as bone and frozen.
- surgical instruments which must be sterilized frequently, which leads to severe corrosion in instruments not coated according to the invention after a short time due to the sterilization conditions (heat, humidity and pressure).
- the suitability of the instrument is impaired as such, and on the other hand suffers in particular the sharpness of the blades used heavily.
- Cylinder the sealing elements and the surfaces of rods and cylinders.
- Engine units and components in particular pistons with or without piston rings, liners and cylinder liners, valves and camshafts, pistons and connecting rods.
- Prostheses implants, screws, plates, artificial joints, stents, biomechanical and micromechanical components.
- Operative cutlery which generally have to be anti-allergenic, such as scalpels, forceps, endoscopes, cutting instruments, staples etc.
- Components which must have chemically resistant surfaces against printable inks and cleaning agents and whose surfaces require defined non-stick and liquid-repellent and / or liquid-adhering properties for defined ink dosing, such as rollers, cylinders and scrapers of printing presses.
- Moving media guides for gas, liquids and gas or liquid fluidized solid media • Moving media guides for gas, liquids and gas or liquid fluidized solid media.
- workpieces and / or materials to be coated according to the invention include cutting, drilling and screwing tools, cutting tools, ball or roller bearings, gears, pinions, drive chains, sound and drive units in magnetic recording devices, as well as surgical and dental surgical instruments
- Standard cubic centimeters per minute and represents a standardized volume flow. In vacuum pump technology, one also speaks of the gas load. Regardless of pressure and Temperature is detected with this standard a defined flowing gas quantity (particle number) per unit time.
- a butcher blade coated with the described method had a threefold service life in comparison to a conventional coater knife with combination coating.
- An industrial cutting knife for potatoes coated with the described method exhibited an eight times longer service life than a conventional cutting knife with a combination coating.
- a punching tool coated with the described method for the production of electrical connectors for the automotive industry had a two-fold extended service life compared to a conventional punching tool.
- Fig. 1 shows a timing chart of the course of the ramps described in Table 4.
- the first block shows the sputtering step (a.2), while the second block shows the step b) for the application the adhesive layer and the ramp-like toothing of the same with the applied in step c) cover layer.
- step (a.2) - or even instead of the sputtering step (a.2) - step (a.1) can be connected for the application of a support layer.
- This step may e.g. the application of a method selected from the group
- FIGS. 2 to 4 show the results of the physical analysis of three stainless steel workpieces, one of which is provided with a titanium nitride coating ("TiN”) and two further coatings according to the invention ("M44", layer thickness 0.81 ⁇ m, "M59”). , Layer thickness 0.84 ⁇ m, layer structure: DLC cover layer with adhesive layer on a HVOF coating of metal-bonded tungsten carbide type WC-Co 83 17). Titanium nitride is considered in the art as one of the hardest and most resistant coatings for cutting, milling and punching tools.
- Counter body WC co-ball, diameter 6 mm
- Friction track diameter D 2 mm
- Fig. 2 shows the results of the determination of the friction coefficient ⁇ . It can be clearly seen that the coating according to the invention with an average coefficient of friction ⁇ of approximately 0.3 has significant advantages over the TiN coating, whose mean coefficient of friction is almost twice as high throughout.
- FIG. 3 shows the light microscopic documentation (magnification: 100 ⁇ ) of the wear in the rubbing track after 30,000 revolutions in the case of the coating M59 according to the invention (FIG. 3 a) and of the TiN coating (FIG. 3 b). It is clearly evident here that the coating according to the invention shows significantly lower wear than the TiN coating.
- FIG. 5 shows an electron micrograph of a section of a workpiece coated according to the invention at a magnification of 3000 times.
- the DLC layer 1 the bright line emerging adhesive layer 2 and the support layer 3 (here a HVOF support layer).
- the DLC layer has a thickness of about 4 ⁇ m. It is also clear that the embedding medium adheres poorly to the DLC layer; Thus, the DLC layer has separated during the cutting of the embedding medium (gap 4). It can also be seen that the DLC coating applied by the plasma coating method is able to compensate for unevennesses (5) of the previously applied supporting layer.
Landscapes
- Chemical & Material Sciences (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Chemical Vapour Deposition (AREA)
- Coating By Spraying Or Casting (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Laminated Bodies (AREA)
Abstract
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007017891 | 2007-04-13 | ||
DE200710047629 DE102007047629A1 (de) | 2007-04-13 | 2007-10-04 | Verfahren zum Aufbringen einer hochfesten Beschichtung auf Werkstücke und/oder Werkstoffe |
PCT/EP2008/054394 WO2008125607A2 (fr) | 2007-04-13 | 2008-04-11 | Procédé d'application d'un revêtement à résistance élevée sur des pièces à usiner et/ou des matériaux |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2134884A2 true EP2134884A2 (fr) | 2009-12-23 |
EP2134884B1 EP2134884B1 (fr) | 2012-08-01 |
Family
ID=39744354
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20080736109 Active EP2134884B1 (fr) | 2007-04-13 | 2008-04-11 | Procédé d'application d'un revêtement à résistance élevée sur des pièces à usiner et/ou des matériaux |
Country Status (11)
Country | Link |
---|---|
US (2) | US20090011252A1 (fr) |
EP (1) | EP2134884B1 (fr) |
JP (1) | JP2010523824A (fr) |
KR (1) | KR20100016486A (fr) |
CN (1) | CN101711288A (fr) |
AU (1) | AU2008237924A1 (fr) |
CA (2) | CA2629117A1 (fr) |
DE (2) | DE102007047629A1 (fr) |
RU (1) | RU2009137553A (fr) |
WO (2) | WO2008125606A1 (fr) |
ZA (1) | ZA200907082B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102018102419A1 (de) * | 2018-02-02 | 2019-08-08 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Passives elektrisches Bauteil mit einer Indikatorschicht und einer Schutzbeschichtung |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4066440B2 (ja) * | 2006-05-17 | 2008-03-26 | トーヨーエイテック株式会社 | ダイヤモンド様薄膜を備えた医療器具及びその製造方法 |
DE102007047629A1 (de) * | 2007-04-13 | 2008-10-16 | Stein, Ralf | Verfahren zum Aufbringen einer hochfesten Beschichtung auf Werkstücke und/oder Werkstoffe |
US8128887B2 (en) * | 2008-09-05 | 2012-03-06 | Uop Llc | Metal-based coatings for inhibiting metal catalyzed coke formation in hydrocarbon conversion processes |
TW201020336A (en) * | 2008-11-20 | 2010-06-01 | Yu-Hsueh Lin | Method for plating film on surface of heat dissipation module and film-plated heat dissipation module |
DE102009008271A1 (de) | 2009-02-10 | 2010-08-12 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zum Beschichten eines Substrats mit einem kohlenstoffhaltigen Hartstoff |
WO2010092616A1 (fr) * | 2009-02-10 | 2010-08-19 | 国立大学法人広島大学 | Matériau d'implant et son procédé de production |
JP5469553B2 (ja) * | 2009-07-17 | 2014-04-16 | 日本碍子株式会社 | アンモニア濃度検出センサ |
IT1396884B1 (it) * | 2009-12-15 | 2012-12-20 | Nuovo Pignone Spa | Inserti in carburo di tungsteno e metodo |
CN101880876B (zh) * | 2010-07-06 | 2012-01-25 | 星弧涂层科技(苏州工业园区)有限公司 | 压缩机滑片及其表面涂层处理方法 |
BRPI1100176A2 (pt) * | 2011-02-10 | 2013-04-24 | Mahle Metal Leve Sa | componente de motor |
DE102011115759B4 (de) * | 2011-10-12 | 2015-10-01 | Thyssenkrupp Industrial Solutions Ag | Keramikkörper, Verfahren zu seiner Herstellung und Verwendung eines Beschichtungsmaterials |
JP2013227626A (ja) * | 2012-04-26 | 2013-11-07 | Kojima Press Industry Co Ltd | Cvd膜の形成方法並びに積層構造体 |
BR102012012636B1 (pt) * | 2012-05-25 | 2022-01-04 | Mahle Metal Leve S/A | Cilindro para aplicação em um motor de combustão interna |
US9765726B2 (en) | 2013-03-13 | 2017-09-19 | Federal-Mogul | Cylinder liners with adhesive metallic layers and methods of forming the cylinder liners |
BR102013031497A2 (pt) * | 2013-12-06 | 2015-11-10 | Mahle Int Gmbh | processo de revestimento de um cilindro de um motor a combustão interna e cilindro/camisa de motor |
DE112015002677T5 (de) * | 2014-06-06 | 2017-03-09 | National Research Council Of Canada | Doppellagenmetallbeschichtung eines Leichtmetallsubstrats |
RU2563910C1 (ru) * | 2014-07-01 | 2015-09-27 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Кубанский государственный технологический университет" (ФГБОУ ВПО "КубГТУ") | Технологическая вакуумная установка для получения наноструктурированных покрытий из материала с эффектом памяти формы на поверхности детали |
US9190266B1 (en) | 2014-08-27 | 2015-11-17 | The Regents Of The University Of California | High capacitance density gate dielectrics for III-V semiconductor channels using a pre-disposition surface treatment involving plasma and TI precursor exposure |
US9873180B2 (en) * | 2014-10-17 | 2018-01-23 | Applied Materials, Inc. | CMP pad construction with composite material properties using additive manufacturing processes |
CN105500823A (zh) * | 2014-10-15 | 2016-04-20 | 深圳富泰宏精密工业有限公司 | 金属与树脂的复合体的制备方法 |
DE102015100441A1 (de) * | 2015-01-13 | 2016-07-14 | Airbus Defence and Space GmbH | Struktur oder Bauteil für Hochtemperaturanwendungen sowie Verfahren und Vorrichtung zur Herstellung derselben |
GB2535481A (en) * | 2015-02-17 | 2016-08-24 | Skf Ab | Electrically insulated bearing |
WO2016146735A1 (fr) * | 2015-03-19 | 2016-09-22 | Höganäs Ab (Publ) | Nouvelle composition de poudre et son utilisation |
CN108135356B (zh) * | 2015-09-07 | 2021-01-08 | 宜家供应有限公司 | 抽屉和用于这种抽屉的抽屉滑动系统 |
CN105483695B (zh) * | 2015-12-04 | 2018-03-30 | 武汉钢铁重工集团有限公司 | 一种炉底辊的制作方法 |
DE102017200543A1 (de) | 2017-01-13 | 2018-07-19 | Baden-Württemberg Stiftung Ggmbh | Verfahren zur Behandlung einer Oberfläche eines Hartmetallkörpers und zur Beschichtung des behandelten Hartmetallkörpers mit einer Diamantschicht |
KR101944906B1 (ko) * | 2017-02-14 | 2019-02-01 | 조선이공대학교 산학협력단 | 가속도 센서축 분해능 향상을 위한 저가 초박형 크롬 도핑 탄소봉 |
SE540785C2 (en) | 2017-03-03 | 2018-11-13 | Ikea Supply Ag | A furniture rotary system having reduced friction, and a piece of furniture comprising such system |
CN107043936A (zh) * | 2017-03-24 | 2017-08-15 | 纳狮新材料股份有限公司 | 复合涂层齿圈及其制备方法 |
CN109723512A (zh) * | 2017-10-30 | 2019-05-07 | 丹阳市金长汽车部件有限公司 | 一种发动机凸轮轴 |
DE102017130449B4 (de) * | 2017-12-14 | 2021-01-21 | Schaeffler Technologies AG & Co. KG | Stempelwerkzeug zum Reibnieten |
CN110564334B (zh) * | 2018-06-05 | 2022-01-04 | 德莎欧洲股份公司 | 低温反应固化型粘合剂的耐湿热性和耐化学试剂腐蚀性的提高 |
US11643730B2 (en) * | 2019-06-28 | 2023-05-09 | Schlumberger Technology Corporation | Anti-scale deposition hierarchical coatings for wellbore applications |
CN111763901A (zh) * | 2020-07-03 | 2020-10-13 | 山东昌丰轮胎有限公司 | 一种带有防粘涂层的轮胎模具 |
CN112410719B (zh) * | 2020-10-20 | 2023-01-20 | 安徽华飞机械铸锻有限公司 | 一种抗磨性的耐热钢 |
CN113388833B (zh) * | 2021-05-31 | 2022-06-03 | 四川大学 | 一种抗冲蚀磨损的流体阀门零件制备方法 |
CN114538930B (zh) * | 2022-03-23 | 2023-01-17 | 山东大学 | 一种裂纹自愈合梯度功能陶瓷刀具材料及其制备方法 |
EP4391719A1 (fr) * | 2022-12-23 | 2024-06-26 | JT International SA | Procédé de production d'un dispositif de chauffage pour un dispositif de génération d'aérosol, dispositif de chauffage pour un dispositif de génération d'aérosol et dispositif de génération d'aérosol |
CN116179883B (zh) * | 2022-12-28 | 2024-06-25 | 吉林大学 | 一种纳米NbB2颗粒增强NiAl合金制备方法 |
CN116162931B (zh) * | 2023-04-26 | 2023-08-04 | 中国恩菲工程技术有限公司 | 一种底吹喷枪复合涂层及其制备方法和底吹喷枪 |
TWI818889B (zh) * | 2023-05-31 | 2023-10-11 | 抱樸科技股份有限公司 | 在具有奈米結構的模具上製作抗沾黏膜的方法 |
CN116590707A (zh) * | 2023-07-14 | 2023-08-15 | 苏州瑞德智慧精密科技股份有限公司 | 一种注塑模具制备dlc涂层的方法及注塑模具 |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4503125A (en) * | 1979-10-01 | 1985-03-05 | Xebec, Inc. | Protective overcoating for magnetic recording discs and method for forming the same |
EP0089382B1 (fr) * | 1982-03-18 | 1986-08-20 | Ibm Deutschland Gmbh | Réacteur à plasma et son utilisation pour graver et revêtir des substrats |
JPS5957416A (ja) * | 1982-09-27 | 1984-04-03 | Konishiroku Photo Ind Co Ltd | 化合物半導体層の形成方法 |
JP2938552B2 (ja) * | 1990-10-17 | 1999-08-23 | 富士通株式会社 | コーティング膜の製造方法およびコーティング膜の製造装置 |
DE4226914A1 (de) * | 1992-08-14 | 1994-02-17 | Basf Magnetics Gmbh | Magnetischer Aufzeichnungsträger |
DE19808180A1 (de) * | 1998-02-26 | 1999-09-09 | Bosch Gmbh Robert | Kombinierte Verschleißschutzschicht, Verfahren zur Erzeugung derselben, die damit beschichteten Objekte und deren Verwendung |
WO2000015869A1 (fr) * | 1998-09-11 | 2000-03-23 | Commissariat A L'energie Atomique | Piece a base d'aluminium revetue de carbone dur amorphe |
DE10018143C5 (de) * | 2000-04-12 | 2012-09-06 | Oerlikon Trading Ag, Trübbach | DLC-Schichtsystem sowie Verfahren und Vorrichtung zur Herstellung eines derartigen Schichtsystems |
JP3630073B2 (ja) * | 2000-05-17 | 2005-03-16 | セイコーエプソン株式会社 | 半導体装置の製造方法 |
JP2002005013A (ja) * | 2000-06-27 | 2002-01-09 | Toyota Industries Corp | 斜板式圧縮機 |
DE10126118A1 (de) | 2001-05-29 | 2002-12-12 | Saxonia Umformtechnik Gmbh | Modifizierter DLC-Schichtaufbau |
DE10213661A1 (de) * | 2002-03-27 | 2003-10-16 | Bosch Gmbh Robert | Verfahren zur Herstellung einer Beschichtung eines metallischen Substrates |
EP1422308B1 (fr) * | 2002-11-22 | 2008-03-26 | Sulzer Metco (US) Inc. | Poudre de pulvérisation pour la fabrication par pulvérisation thermique d'un revêtement de barrière thermique résistant à haute température |
DE10331785B4 (de) * | 2003-07-11 | 2007-08-23 | H. C. Starck Gmbh & Co. Kg | Verfahren zur Herstellung feiner Metall-, Legierungs-und Verbundpulver |
EP1518622A1 (fr) * | 2003-09-26 | 2005-03-30 | Sulzer Metco (US) Inc. | Procédé pour la préparation de granulats contenant de matière dure |
IL166652A (en) * | 2004-03-12 | 2010-11-30 | Sulzer Metaplas Gmbh | Carbon containing hard coating and method for depositing a hard coating onto a substrate |
DE102004032342B4 (de) * | 2004-07-03 | 2006-06-08 | Federal-Mogul Burscheid Gmbh | Kolbenring mit mindestens zwei unterschiedlichen Schichten auf der Lauffläche |
EP1771596A1 (fr) * | 2004-07-09 | 2007-04-11 | OC Oerlikon Balzers AG | MATERIAU CONDUCTEUR A BASE DE CUIVRE PRESENTANT UN REVETEMENT EN MATERIAU DUR Me-DLC |
DE102005055064A1 (de) | 2005-11-16 | 2007-05-24 | Kipp, Jens Werner | Strahlvorrichtung für die Reinigung und Entschichtung langer Gegenstände wie z.B.Drähte, Bänder, Stangen, Ketten, aneinander hängende Stanzteile |
DE102006032568A1 (de) * | 2006-07-12 | 2008-01-17 | Stein, Ralf | Verfahren zur plasmagestützten chemischen Gasphasenabscheidung an der Innenwand eines Hohlkörpers |
DE102007047629A1 (de) * | 2007-04-13 | 2008-10-16 | Stein, Ralf | Verfahren zum Aufbringen einer hochfesten Beschichtung auf Werkstücke und/oder Werkstoffe |
DE102007020852A1 (de) | 2007-05-02 | 2008-11-06 | Stein, Ralf | Gasversorgungssystem und Verfahren zur Bereitstellung eines gasförmigen Abscheidungsmediums |
-
2007
- 2007-10-04 DE DE200710047629 patent/DE102007047629A1/de not_active Withdrawn
- 2007-12-04 DE DE200710058484 patent/DE102007058484A1/de not_active Withdrawn
-
2008
- 2008-04-10 CA CA 2629117 patent/CA2629117A1/fr not_active Abandoned
- 2008-04-10 US US12/100,668 patent/US20090011252A1/en not_active Abandoned
- 2008-04-11 US US12/595,355 patent/US20100297440A1/en not_active Abandoned
- 2008-04-11 WO PCT/EP2008/054391 patent/WO2008125606A1/fr active Application Filing
- 2008-04-11 JP JP2010502515A patent/JP2010523824A/ja active Pending
- 2008-04-11 EP EP20080736109 patent/EP2134884B1/fr active Active
- 2008-04-11 AU AU2008237924A patent/AU2008237924A1/en not_active Abandoned
- 2008-04-11 RU RU2009137553/02A patent/RU2009137553A/ru not_active Application Discontinuation
- 2008-04-11 KR KR20097023632A patent/KR20100016486A/ko not_active Application Discontinuation
- 2008-04-11 CN CN200880015676A patent/CN101711288A/zh active Pending
- 2008-04-11 WO PCT/EP2008/054394 patent/WO2008125607A2/fr active Application Filing
- 2008-04-11 CA CA 2684019 patent/CA2684019A1/fr not_active Abandoned
-
2009
- 2009-10-12 ZA ZA200907082A patent/ZA200907082B/xx unknown
Non-Patent Citations (1)
Title |
---|
See references of WO2008125607A2 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102018102419A1 (de) * | 2018-02-02 | 2019-08-08 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Passives elektrisches Bauteil mit einer Indikatorschicht und einer Schutzbeschichtung |
Also Published As
Publication number | Publication date |
---|---|
JP2010523824A (ja) | 2010-07-15 |
CA2629117A1 (fr) | 2008-10-13 |
WO2008125606A1 (fr) | 2008-10-23 |
CN101711288A (zh) | 2010-05-19 |
US20090011252A1 (en) | 2009-01-08 |
RU2009137553A (ru) | 2011-04-20 |
WO2008125607A2 (fr) | 2008-10-23 |
CA2684019A1 (fr) | 2008-10-23 |
DE102007058484A1 (de) | 2008-10-16 |
AU2008237924A1 (en) | 2008-10-23 |
WO2008125607A3 (fr) | 2009-05-07 |
ZA200907082B (en) | 2010-07-28 |
DE102007047629A1 (de) | 2008-10-16 |
EP2134884B1 (fr) | 2012-08-01 |
KR20100016486A (ko) | 2010-02-12 |
US20100297440A1 (en) | 2010-11-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2134884B1 (fr) | Procédé d'application d'un revêtement à résistance élevée sur des pièces à usiner et/ou des matériaux | |
EP2668309B1 (fr) | Élément coulissant, notamment segment de piston avec un revêtement et procédé de fabrication d'un élément coulissant | |
DE19518781C1 (de) | Vakuumbeschichteter Verbundkörper und Verfahren zu seiner Herstellung | |
EP2209929B1 (fr) | Outil revetu | |
EP2912206B1 (fr) | Composant doté d'un revêtement et procédé pour le fabriquer | |
DE602004003547T2 (de) | Verfahren zur Beschichtung eines Schneidwerkzeuges. | |
WO2005106065A1 (fr) | Revetement en un materiau dur dlc sur des materiaux a teneur en cuivre pour paliers | |
EP3423609A1 (fr) | Revêtement en carbone exempt d'hydrogène comprenant une couche adhésive de zirconium | |
EP3929325A1 (fr) | Procédé de fabrication d'un cible de dépôt physique en phase vapeur (pvd) et cible de crta obtenu | |
EP1980645A1 (fr) | Procédé d'application d'un revêtement multicouche sur des pièces à usiner et/ou matières actives | |
AT5008U1 (de) | Hartmetallverschleissteil mit mischoxidschicht | |
DE102012020756A1 (de) | Bauteil mit einer Beschichtung und Verfahren zu seiner Herstellung | |
EP0724023A1 (fr) | Couches carbonées dures, amorphes et exemptes d'hydrogène | |
EP2454393B1 (fr) | Procédé de fabrication de plaquettes amovibles | |
EP0832993A1 (fr) | Système de couches, procédé pour sa fabrication et substrat métallique avec un tel système de couches | |
EP2396448B1 (fr) | Procédé pour appliquer un revêtement sur des pièces et/ou des matériaux présentant au moins un métal non-ferreux facilement oxydable | |
WO2013023802A1 (fr) | Couche de lissage pour pièces métalliques | |
DE10149588A1 (de) | Verfahren zur Diamantbeschichtung von Substraten | |
EP0348389A1 (fr) | Couche de glissement pour endoprotheses d'articulations et son procede de production | |
DE19506656B4 (de) | Verfahren zur Keramisierung von Leichtmetalloberflächen | |
Sheveyko et al. | Hybrid Technology Combining Vacuum Electrospark Alloying, Cathodic Arc Evaporation, and Magnetron Sputtering for the Deposition of Hard Wear-Resistant Coatings | |
Kumari | Study of TiC coating on different type steel by electro discharge coating | |
EP1522610B1 (fr) | Procédé de production d'une couche de protection contre l'usure | |
AT523638B1 (de) | Verfahren zur Herstellung einer Hartstoffschicht auf einer Metalloberfläche | |
Slomski et al. | Effect of PVD process parameters on nucleation and structure of CrN layers |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20091105 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR |
|
17Q | First examination report despatched |
Effective date: 20100413 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
DAX | Request for extension of the european patent (deleted) | ||
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP Ref country code: AT Ref legal event code: REF Ref document number: 568769 Country of ref document: AT Kind code of ref document: T Effective date: 20120815 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
RAP2 | Party data changed (patent owner data changed or rights of a patent transferred) |
Owner name: SURCOATEC AG |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502008007832 Country of ref document: DE Effective date: 20120927 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: VDEP Effective date: 20120801 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D Effective date: 20120801 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20121201 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20121101 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20121203 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20121102 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20121112 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20130503 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20121101 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502008007832 Country of ref document: DE Effective date: 20130503 |
|
BERE | Be: lapsed |
Owner name: STEIN, RALF Effective date: 20130430 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130430 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130411 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120801 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130411 Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20080411 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 9 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20170419 Year of fee payment: 10 Ref country code: GB Payment date: 20170419 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 20170420 Year of fee payment: 10 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 568769 Country of ref document: AT Kind code of ref document: T Effective date: 20180411 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20180411 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180411 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180411 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180430 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PK Free format text: DIE LOESCHUNG VOM 21.11.22 ERFOLGTE IRRTUEMLICH. Ref country code: CH Ref legal event code: PK Free format text: BERICHTIGUNGEN |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20240529 Year of fee payment: 17 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20240523 Year of fee payment: 17 |